Flight Dynamics, Control, and Testing of a Coaxial Helicopter UAV with Folding Rotor Blades

F-0079-2023-18189

5/16/2023

Authors
Abstract
Content

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Pages
13
Citation
Gong, A., Tischler, M., and Shalev-Eggert, O., "Flight Dynamics, Control, and Testing of a Coaxial Helicopter UAV with Folding Rotor Blades," Vertical Flight Society 79th Annual Forum and Technology Display, West Palm Beach, Florida, May 16, 2023, .
Additional Details
Publisher
Published
5/16/2023
Product Code
F-0079-2023-18189
Content Type
Technical Paper
Language
English